N659FE

Service difficulty reports · 213

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N659FE' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201706231747Power Supply · damagedFORWARD CABIN OVERHEAD EMERGENCY EXIT LIGHTS FLICKER ON AND OFF DURING TURBULENT CONDITIONS, CLIMB, AND DESCENT. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW AMM 33-51-14-04. OPS CHECKED GOOD. OK FOR SERVICE.Jun 23, 2017 · N659FE · Airbus A300F4605R · Emergency LightingSDR FDEA201610113543Cargo Track · corrodedCARGO TRACK SCALLOP DAMAGED. REMOVED CORROSION IAW SRM 51-74-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG.102. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 53-10-16 FIG.201. MAJOR REPAIR.Oct 11, 2016 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201610113542Static Wick · detachedLEFT OUTBD FLAP OUTBD STATIC WICK BASE DETACHED. REPAIRED IAW EA 6-5750-T0328567. MAJOR REPAIR.Oct 11, 2016 · N659FE · Airbus A300F4605R · Static Discharge SystemSDR FDEA201610073497Floor Panel · damagedAFT CARGO FLOOR PANEL 151QF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 AND INSTALLED. MAJOR REPAIR.Oct 7, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610073496Floor Panel · damagedAFT CARGO FLOOR PANEL 151UF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-025-005 AND INSTALLED. MAJOR REPAIROct 7, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610073494Floor Panel · damagedAFT CARGO FLOOR PANEL 151RF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 AND INSTALLED. MAJOR REPAIR.Oct 7, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610073492Floor Panel · damagedFWD CARGO FLOOR PANEL 132NG DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 & INSTALLED. MAJOR REPAIR.Oct 7, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610073491Floor Panel · damagedAFT CARGO FLOOR PANEL 152TF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 AND INSTALLED. MAJOR REPAIR.Oct 7, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610073490Floor Panel · damagedFWD CARGO FLOOR PANEL 131SG DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 AND INSTALLED. MAJOR REPAIR.Oct 7, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610073489Floor Panel · damagedAFT CARGO FLOOR PANEL 151XF DAMAGED / BROKEN. FABRICATED AFT CARGO FLOOR PANEL 151XF ON VTMAE TRAVELER # T16/1230926 IAW SRZ 25- 005 & INSTALLED ON WORK CARD 150-FL-FIT. MAJOR REPAIROct 7, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610073488Floor Panel · damagedAFT CARGO FLOOR PANEL 152UF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 & INSTALLED. MAJOR REPAIROct 7, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610073484Floor Panel · damagedFWD CARGO FLOOR PANEL 132SG DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 & INSTALLED.Oct 7, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610073482Floor Panel · damagedFWD CARGO FLOOR PANEL 132PG BROKEN AND DAMAGED. FABRICATED FWD CARGO FLOOR PANEL 132PG ON TRAVELER T16/1231048 IAW SRZ 25-005 AND INSTALLED.Oct 7, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610033441Seat Track · wornMCD #5 DUMMY SEAT TRACK FAILED GAP CHECK REMOVED SEAT TRACK IAW SRM 51-40-21. FABRICATE INSERT ON VT MAE TRAVELER # T16/1231805. RE-WORKED SEAT TRACK ON VT MAE TRAVELER # T16/1231806 IAW SRM 53-15-16 FIG 201. INSTALLED SEAT TRACK IAW SRM 51-40-21. MAJOR REOct 3, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610033440Seat Track · wornMCD LH # 3 DUMMY SEAT TRACK FAILED GAP CHECK REMOVED SEAT TRACK IAW SRM 51-40-21. FABRICATED INSERT ON VT MAE TRAVELER # T16/1231410. RE-WORKED SEAT TRACK ON VT MAE TRAVELER # T16/1231801 IAW SRM 53-15-16 FIG 201. INSTALLED SEAT TRACK IAW SRM 51-40-21. MAJOct 3, 2016 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201610033439Seat Track · wornSEAT TRACK FAILED GAP CHECK. REPLACED THE SEAT TRACK IAW SRM 51-40-21, SRM 53-15-16 FIG 201. MAJOR REPAIR.Oct 3, 2016 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201610013419Floor Panel · crackedMAIN DECK FLOOR PANEL 251VF CRACKED ON TOP SURFACE. FABRICATED FLOOR PANEL 251VF IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013418Floor Panel · puncturedMAIN DECK FLOORBOARD PANEL 231EF IS PUNCTURED. FABRICATED FLOOR PANEL 231EF IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013417Floor Panel · crackedMAIN DECK FLOORBOARD 232CF IS CRACKED ON UPPER SURFACE. FABRICATED FLOOR PANEL 2312CF IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013416Floor Panel · puncturedFLOOR PANEL 231CF PUNCTURED. FABRICATED NEW FLOOR PANEL 231CF IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013415Floor Panel · crackedFLOOR PANEL 242DF CRACKED. FABRICATED NEW FLOOR PANEL 242DF IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013414Floor Panel · brokenMAIN CABIN FLOOR PANEL 231HG BROKEN. FABRICATED NEW FLOOR PANEL 231HG.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013413Floor Panel · crackedMAIN DECK FLOORBOARD PANEL 242ZJ HAS BROKEN INSERTS. FABRICATED NEW FLOOR PANEL 242ZJ IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013412Floor Panel · crackedMAIN DECK FLOORBOARD PANEL 242EK IS CRACKED. FABRICATED NEW FLOOR PANEL 242EK IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013411Floor Panel · damagedMAIN DECK FLOORBOARD PANEL 241HK HAS BROKEN INSERTS. FABRICATED NEW FLOOR PANEL 241HK IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013410Floor Panel · damagedMAIN DECK FLOORBOARD 241QF HAS BROKEN INSERTS. FABRICATED NEW FLOOR PANEL 241QF IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013409Floor Panel · damagedMAIN DECK FLOORBOARD PANEL 241AJ HAS BROKEN INSERTS. FABRICATED NEW FLOOR PANEL 241AJ IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013408Floor Panel · damagedMAIN DECK FLOORBOARD 241NH HAS BROKEN INSERTS. FABRICATED FLOOR BOARD 241NH IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201610013407Floor Panel · crackedMAIN DECK FLOORBOARD PANEL 242GF IS CRACKED ON UPPER SURFACE. FABRICATED NEW FLOOR PANEL 242GF IAW SRM 25-005. MAJOR REPAIR.Oct 1, 2016 · N659FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201609293393Seat Track · gougedGOUGES ON SEAT TRACK SCALLOP IN MD CARGO BAY FRAME 62, Y1956. BLENDED DAMAGE AREA WITH A MATERIAL LOSS OF .110" , MAX. ALLOWED .028" OUT OF LIMITS IAW SRM 53-10-16 FIG.102 VERIFIED BY TR14402 REPAIRED DAMAGED SEAT TRACK IAW SRM 53-10-16 FIG.201 THIS IS A CATSep 29, 2016 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609293390Floor Support · corrodedMAIN DECK FROM FRAMES 12 TO 13 FLOOR SUPPORT Y730 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21 AT Y730 CLASSIFIED AS A MAJOR REPAIR.Sep 29, 2016 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201609103191Transmitter · out of adjustDURING FLIGHT CONTROL CHECK, AT FULL THROW RIGHT RUDDER STUCK AT FULL RUDDER POSITION. AFTER A FEW SECONDS IT CAME BACK TO NEUTRAL AFTER A BANG AND A GRINDING NOISE. THE ROD CONNECTED TO THE RUDDER SENSOR BINDING, AND STICKING ON BRACKET, ON THE CAPTAISep 10, 2016 · N659FE · Airbus A300F4605R · Rudder Control SystemSDR FDEA201608263004Clamp · looseON FLIGHT CONTROL CHECK BEFORE T/O, RUDDER STICKS RT WHEN RT RUDDER APPLIED. WILL NOT RETURN TO CENTER. PEDALS ARE DISPLACED AS WELL BOTH CAPTAIN AND F/O SIDES. RELEASED FOR SERVICE. DFDAU RUDDER POSITION SENSOR CLAMP ON TORQUE TUBE LOOSE ALLOWING SENSOR TOAug 26, 2016 · N659FE · Airbus A300F4605R · Rudder Control SystemSDR FDEA201503040655Rib · corrodedRIGHT MLG FWD LUG HAS CORROSION IN BORE & ON AFT FACE. REPAIRED IAW DWG R572-40425 REV D & EA 6-5710-T0315862 P 1. TERMINATING ACTION OF RIB 5 FWD LUG RT. CAT C MAJOR REPAIR.Mar 4, 2015 · N659FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201503040654Rib · corrodedLEFT MLG FWD LUG HAS CORROSION IN BORE & FWD & AFT FACES. COMPLIED WITH REPAIR DWG R572-40425 REV D & EA 6-5710-T0315858 P1-WINGS, BASIC WING STRUCTURE, TERMINATING ACTION LT RIB 5 FWD LUG CAT C MAJOR REPAIR.Mar 4, 2015 · N659FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201406171476Structure · crackedLEFT ENGINE OTBD THRUST REVERSER COWL FWD SUPPORT FRAME WEB FOUND CRACKED AT ABOUT 12:00 POSITION. REPAIRED IAW EA 6-7830-T0308498 PT 1. MAJOR REPAIR IAW GMM6-2-100.Jun 17, 2014 · N659FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201406111397Rib · crackedLEFT WING CTR FLAP UPPER SKIN LOWER SUPPORT RIB 26 FOUND CRACKED AT ABOUT STRINGER 2.8. REPAIRED IAW EA 6-5750-T0308432 PT1. MAJOR REPAIR IAW GMM6-2-100.Jun 11, 2014 · N659FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201406111398Rib · crackedLEFT WING CENTER FLAP UPPER SKIN LOWER SUPPORT RIB 27 FOUND CRACKED IN THREE PLACES. REPAIRED IAW EA 6-5750-T0308432 PT1. MAJOR REPAIR IAW GMM6-2-100.Jun 11, 2014 · N659FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201406011253Skin · crackedLEFT WING CTR FLAP UPPER SKIN FOUND CRACK BETWEEN RIB 26 - 27, STRINGERS 2.7 - 2.8. COMPLETED EA 6-5750-T0308432 PT1. MAJOR REPAIR IAW GMM6-2-100.Jun 1, 2014 · N659FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201405211111Fitting · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING BETWEEN FRAMES 40 - 44 CRACKED. REAMED IAW SRM 51-40-44. ROTO-TEST INSPECTION IAW NTM51-10-01. NO CRACK FOUND,AND INSTALL NEW FASTENERS IAW SRM 51-40-21. COMPLIED WITH EA 6-5710-T0308783 P1. MAJOR REPAIR IMay 21, 2014 · N659FE · Airbus A300F4605R · Wing Main, Frame StructureSDR FDEA201405211112Fitting · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING BETWEEN FRAMES 40 - 44 CRACKED. REAMED IAW SRM 51-40-44. ROTO-TESTED INSPECTION IAW NTM51-10-01. NO CRACK FOUND. INSTALLED NEW FASTENERS IAW SRM 51-40-21. COMPLIED WITH EA 6-5710-T0308783 PT1. MAJOR REPAMay 21, 2014 · N659FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201405211108Frame · crackedCENTER WING JOINT AT FRAME 40 RT HAD A CRACK SIGNAL. REAMED THE HOLE TO REMOVE THE DAMAGE AND COMPLIED WITH EA 6-5710-T0308852 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 21, 2014 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201405211107Frame · crackedCENTER WING JOINT AT FRAME 40 RT SIDE WITH A CRACK SIGNAL. REAMED THE HOLE TO REMOVE THE CRACK AND COMPLIED WITH EA6-5710-T0308852 PT1. MAJOR REPAIR IAW GMM6-2-100.May 21, 2014 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201405211110Frame · crackedFRAME 47 SPLICE FITTING BETWEEN STRINGERS 24 & 26R CRACKED. REPAIRED IAW EO 6-5310-7-5017 PT6. MAJOR REPAIR IAW GMM 6-2-100.May 21, 2014 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201405211109Frame · crackedFRAME 47, SPLICE FITTING BETWEEN STRINGER 24 & 26L CRACKED. REPAIRED IAW EO6-5310-7-5017 PT5. MAJOR REPAIR IAW GMM6-2-100.May 21, 2014 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201312062931Transmitter · failedAFTER TAKEOFF RECEIVED THE FOLLOWING ECAM ALERTS & FAILURES. AUTO THROTTLES TRIPPED OFF AT APPROX 120 KTS, YAW DAMPER 2, RESET BUT TRIPPED ON APPROACH. SLATS SYS 1 FAULT, SPOILER 7, 5, 3 & 2 FAULT. CAPTAIN HAD A SPD LIM RED FLAG ON PFD AIRSPEED. OIL PRESS ODec 6, 2013 · N659FE · Airbus A300F4605R · Engine Oil PressureSDR FDEA201307181598Pitot Tube · obstructedREJECTED TAKE OFF AT 95 KIAS DUE TO NO AIRSPEED INDICATION ON CAPTAIN'S PFD. NO TREND ARROW NOR INDICATED AIRSPEED MOVEMENT. FOUND INSECT BLOCKAGE ON CAPTAIN'S PITOT TUBE. CLEARED AND BLEW TUBE OUT WITH NITROGEN. PERFORMED EFIS INPUTS TEST. ALL COMPUTERSJul 18, 2013 · N659FE · Airbus A300F4605R · Airspeed/Mach IndicatorSDR FDEA201305241079Rectifier · burnedNR 1 OIL PRESSURE WENT TO ZERO AFTER TAKEOFF, LOST ATS & YAW DAMPER FAILED AT ROTATION. DID NOT LOSE ANY OIL QTY. ELECTED TO SHUTDOWN NR 1 AND RETURN TO DEPARTURE. NR 1 ENG WINDMILLED APPROX 30 MINUTES YAW DAMPER RESET BUT ATS SYS WOULD NOT. COMPLIED WITHMay 24, 2013 · N659FE · Airbus A300F4605R · Electrical Power SystemSDR FDEA201211154035Control Unit · malfunctionedNR 7 WHEEL BRAKE HEATED UP TO 355 C DURING END OF TAKEOFF. KEPT GEAR DOWN AND CLIMBED TO FL300 AND THE TEMP REMAINED ABOVE 150 C FOR NEXT 22 MINUTES. FINALLY TEMP COOLED OFF TO 25C AFTER A TOTAL OF 30 MINUTES WITH GEAR DOWN. RAISED GEAR AND DIVERTED, NO HONov 15, 2012 · N659FE · Airbus A300B4622 · Landing Gear Brake SystemSDR FDEA201203301197Skin · dentedRIGHT AILERON T/E LOWER SKIN HAS A DENT. FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11, FIG 103. REMOVED DAMAGED AREA OF SKIN, APPLIED FILLER AND BONDED DOUBLER TO LOWER SURFACE IAW SRM 57-61-11, PB 201, PAR 4 E. (1) (A). COMPLIED WITH EA 6-5750-157830.Mar 30, 2012 · N659FE · Airbus A300F4605R · Ailerons
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